MS24515 Revision F:1979
Withdrawn
Withdrawn
LAMPS, INCANDESCENT, T-1, SUB-MIDGET, FLANGED (NO S/S DOCUMENT)
Available format(s)
PDF
Language(s)
English
Published date
05-24-1979
Publisher
Withdrawn date
09-28-1995
Excluding Tax where applicable
| DocumentType |
Standard
|
| Pages |
2
|
| PublisherName |
US Military Specs/Standards/Handbooks
|
| Status |
Withdrawn
|
| Supersedes |
| MIL-I-18856 Revision B:1969 | Indicator, Angle of Attack, 28V DC MS28062 and MS28067 |
| MIL-L-25467 Revision D:1977 | Lighting, Integral, Red, Aircraft Instrument, General Specification for |
| MIL S 24317 : 0 | SWITCH, MULTI-STATION, PUSHBUTTON (ILLUMINATED AND NON-ILLUMINATED), GENERAL SPECIFICATION FOR |
| MIL-I-27191 Revision C:1995 | Indicator, Position, Variable Nozzle |
| MIL-C-27298 Revision B:1980 | Clock, Aircraft, Mechanical ABU-9-A |
| MIL-I-27709 Revision A:1962 | Indicator, Altitude, ARU-14/A, Remote (No S/S Document) |
| MIL-I-27202 Revision A:1980 | Indicator, Electrical Tachometer, 0-110 Percent RPM 2-Inch Size, Integrally Lighted |
| MIL S 22710 : E | SWITCHES, ROTARY (PRINTED CIRCUIT), (THUMBWHEEL, INLINE, AND PUSHBUTTON), GENERAL SPECIFICATION FOR |
| SAE ARP798B | Design Criteria for White Incandescent Lighted Aerospace Instruments |
| MIL-I-21735 Revision A:1969 | Indicator, Airspeed and Mach Number, Pitot Static, 60 to 650 Knots |
| MIL-I-18804 Revision B:1964 | Indicator, Vertical Speed, 0 - 6000 FPM, 2 Inch |
| MIL-I-25931 Revision B:1964 | Indicator, Position, Landing Gear, Symbol-Indicating, Integrally Lighted (No S/S Document) |
| MIL-I-22126 Revision B:1972 | Indicator, Torquemeter, Engine, Turboprop |
| MIL-I-27280 Revision A:1960 | Indicator, Indicated Airspeed AVU-10/A (No S/S Document) |
| MIL-L-27160 Revision C:1972 | Lighting, Instrument, Integral, White, General Specification for |
| MIL-I-27203 Revision B:1987 | Indicator, Position, Wing Flap |
| MIL P 7788 : F | PANEL, INFORMATION INTEGRALLY ILLUMINATED |
| MIL-I-38258 Base Document:1965 | Indicator, Attitude ARU-18/A, Director (No S/S Document) |
| MIL-I-23524 Revision A:1986 | Indicator, Attitude-Director, Remote, ID 1329A (V) |
| MIL-I-23832 Revision A:1980 | Indicator, Tachometer, Triple Pointer, Helicopter |
| MIL-I-81049 Revision A:1972 | Indicator, Temperature, Electrical Resistance, Voltage Compensated, Multifunction (No S/S Document) |
Summarise